JPH0412122A - Fuel collision diffusion type engine - Google Patents

Fuel collision diffusion type engine

Info

Publication number
JPH0412122A
JPH0412122A JP2112645A JP11264590A JPH0412122A JP H0412122 A JPH0412122 A JP H0412122A JP 2112645 A JP2112645 A JP 2112645A JP 11264590 A JP11264590 A JP 11264590A JP H0412122 A JPH0412122 A JP H0412122A
Authority
JP
Japan
Prior art keywords
fuel
combustion chamber
protrusion
flow
squish flow
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP2112645A
Other languages
Japanese (ja)
Inventor
Takaharu Kishishita
敬治 岸下
Hideo Kawamura
英男 河村
Hiroshi Matsuoka
寛 松岡
Yoshio Sekiyama
恵夫 関山
Yoji Sasaki
佐々木 洋士
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Isuzu Motors Ltd
Original Assignee
Isuzu Motors Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Isuzu Motors Ltd filed Critical Isuzu Motors Ltd
Priority to JP2112645A priority Critical patent/JPH0412122A/en
Publication of JPH0412122A publication Critical patent/JPH0412122A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0618Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion
    • F02B23/063Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston having in-cylinder means to influence the charge motion the combustion space in the piston interacting fluid dynamically with the cylinder head, the injector body or the cylinder wall
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0648Means or methods to improve the spray dispersion, evaporation or ignition
    • F02B23/0651Means or methods to improve the spray dispersion, evaporation or ignition the fuel spray impinging on reflecting surfaces or being specially guided throughout the combustion space
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0672Omega-piston bowl, i.e. the combustion space having a central projection pointing towards the cylinder head and the surrounding wall being inclined towards the cylinder center axis
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02BINTERNAL-COMBUSTION PISTON ENGINES; COMBUSTION ENGINES IN GENERAL
    • F02B23/00Other engines characterised by special shape or construction of combustion chambers to improve operation
    • F02B23/02Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition
    • F02B23/06Other engines characterised by special shape or construction of combustion chambers to improve operation with compression ignition the combustion space being arranged in working piston
    • F02B23/0645Details related to the fuel injector or the fuel spray
    • F02B23/0666Details related to the fuel injector or the fuel spray having a single fuel spray jet per injector nozzle
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02FCYLINDERS, PISTONS OR CASINGS, FOR COMBUSTION ENGINES; ARRANGEMENTS OF SEALINGS IN COMBUSTION ENGINES
    • F02F1/00Cylinders; Cylinder heads 
    • F02F1/24Cylinder heads
    • F02F2001/244Arrangement of valve stems in cylinder heads
    • F02F2001/247Arrangement of valve stems in cylinder heads the valve stems being orientated in parallel with the cylinder axis
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/12Improving ICE efficiencies

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Dispersion Chemistry (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Combustion Methods Of Internal-Combustion Engines (AREA)

Abstract

(57)【要約】本公報は電子出願前の出願データであるた
め要約のデータは記録されません。
(57) [Summary] This bulletin contains application data before electronic filing, so abstract data is not recorded.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、燃焼室内に設けた突起体に燃料噴射ノズル
から噴射される燃料を直接衝突させる燃料衝突拡散式エ
ンジンに関する。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a fuel impingement diffusion type engine in which fuel injected from a fuel injection nozzle directly impinges on a protrusion provided within a combustion chamber.

〔従来の技術〕[Conventional technology]

従来、エンジンの燃焼室としては、直接噴射式及び副室
式によって代表されている。
Conventionally, engine combustion chambers are typically of the direct injection type and the pre-chamber type.

直接噴射式燃焼室は、燃料噴射ノズルより噴射された燃
料の噴射エネルギー及び燃焼室内に形成されるスワール
及びスキッシュ流によって燃料と空気との混合を達成し
、可燃性混合気を形成している。しかしながら、該直接
噴射式燃焼室は、スワール生成のため、吸気効率が低下
するという問題を有しており、また、燃料の噴am粒化
及び貫徹力をアンプさせるため、燃料噴射ノズルを高圧
化、高噴射率化に構成しなければならず、構造が複雑に
なるという問題を有している。
A direct injection combustion chamber achieves mixing of fuel and air by the injection energy of fuel injected from a fuel injection nozzle and the swirl and squish flow formed within the combustion chamber to form a flammable mixture. However, the direct injection combustion chamber has the problem of reduced intake efficiency due to swirl generation, and also requires the fuel injection nozzle to be pressurized to amplify the atomization and penetration force of the fuel. However, it has to be configured to have a high injection rate, resulting in a complicated structure.

また、副室式燃焼室は、副室内に形成される高スツール
によって燃料油滴と空気との混合を達成し、可燃性混合
気を形成している。該副室式燃焼室は、副室内に高スワ
ールを形成し、また主室と副室との総和の伝熱面積が増
大して熱損失が増加するという問題があり、更に、主室
と副室とを連通ずる連絡孔による絞り損失が増加すると
いう問題を有している。
Further, in the pre-chamber type combustion chamber, a high stool formed in the pre-chamber achieves mixing of fuel oil droplets and air to form a flammable air-fuel mixture. The pre-chamber type combustion chamber has the problem that a high swirl is formed in the pre-chamber, and the total heat transfer area of the main chamber and the sub-chamber increases, increasing heat loss. There is a problem in that the aperture loss due to the communication hole that communicates with the chamber increases.

そこで、上記問題点を解決するために、燃料の衝突噴流
を利用した直接噴射式衝突拡散層状給気式、いわゆる、
03KA式の燃焼室を持つエンジンが開示されている。
Therefore, in order to solve the above problems, we developed a direct injection collision diffusion stratified air supply system that uses collision jets of fuel.
An engine with a 03KA type combustion chamber is disclosed.

この03KA式エンジンは、ピストンに形成した凹部即
ちキャビティの底部中央から突出する衝突部を設け、該
衝突部の周囲に凹状の燃焼室を形成し、燃料噴射ノズル
から噴射された液状燃料を衝突部に衝突させ、燃料噴流
の衝突部への衝突作用によって衝突面を起点として燃料
の拡散、微粒化等を達成し、燃料と空気との良好な混合
を達成させるものである。上記のような燃焼室を有する
エンジンでは、燃料噴射ノズルの単孔ノズルから噴射さ
れた燃料をピストンヘッドの衝突部の平らな衝突面に衝
突させて円盤状に拡散させ、次いでピストンの上昇によ
って生しるスキッシュ流によって燃料をキャビティの下
方に押し込められながら、該燃料と空気とを混合して混
合気を形成するものである。
This 03KA type engine has a recess formed in the piston, that is, a collision part protruding from the center of the bottom of the cavity, a concave combustion chamber is formed around the collision part, and liquid fuel injected from a fuel injection nozzle is transferred to the collision part. The collision effect of the fuel jet on the collision part causes diffusion and atomization of the fuel starting from the collision surface, thereby achieving good mixing of the fuel and air. In an engine having a combustion chamber as described above, the fuel injected from the single-hole nozzle of the fuel injection nozzle collides with the flat collision surface of the collision part of the piston head and is dispersed in a disk shape, and then the fuel is generated by the rise of the piston. While the fuel is pushed down into the cavity by the squish flow, the fuel and air are mixed to form an air-fuel mixture.

また、特開昭63−120815号公報には、外部点火
による燃料噴射式内燃機関が開示されている。該外部点
火による燃料噴射式内燃機関は、ピストン頂面にキャビ
ティを形成すると共に、該キャビティ内壁面上に突出部
を設け、該突出部上に断熱構造の衝突面を形成し、シリ
ンダヘッドに設けた燃料噴射弁から大部分の燃料を衝突
面に向けて噴射させ、他の領域よりも濃い混合気領域を
上記突出部層りに形成し、点火装置をこの濃い混合気領
域内に位置するようにシリンダヘッドに取付け、該点火
装置で点火時に混合気に点火するものである。該燃料噴
射式内燃機関は、上記の構成によってノンキングが発生
しないことによって高圧縮比を可能にし、熱効率を向上
させて燃料消費率を向上させたものである。
Further, Japanese Patent Application Laid-open No. 120815/1983 discloses a fuel injection type internal combustion engine with external ignition. The fuel injection internal combustion engine with external ignition has a cavity formed on the top surface of the piston, a protrusion on the inner wall surface of the cavity, a collision surface with a heat insulating structure formed on the protrusion, and a cylinder head. Most of the fuel is injected toward the collision surface from the fuel injection valve, forming a richer mixture region than other regions in the protrusion layer, and the ignition device is positioned within this rich mixture region. The ignition device ignites the air-fuel mixture during ignition. The fuel-injected internal combustion engine has the above-described structure, which prevents non-king from occurring, enables a high compression ratio, improves thermal efficiency, and improves fuel consumption.

また、特開昭62−139921号公報には、燃料衝突
反射拡散燃焼方式の内燃機関が開示されている。該内燃
機関は、ノズルより燃料噴流をピストン面又はキャビテ
ィ内に噴射衝突させ、衝突面での反射拡散作用によって
衝突部を起点としてキャビティ全域に燃料の拡散分布と
混合を計り、スワールに依存するよりもスキンシュ流に
よって空気利用率を高め、燃焼期間の短縮を図るもので
あり、衝突部をセラミック材等の耐熱性、耐摩耗性材料
で形成し、該衝突部をピストン頂面又はキャビティ内に
装着したものである。
Furthermore, Japanese Patent Application Laid-open No. 139921/1983 discloses an internal combustion engine using a fuel collision reflection diffusion combustion method. The internal combustion engine uses a nozzle to inject and collide a fuel jet onto the piston surface or into the cavity, and uses the reflection-diffusion effect on the collision surface to measure the diffusion distribution and mixing of the fuel throughout the cavity starting from the collision part, rather than relying on swirl. This method uses skin flow to increase air utilization and shorten the combustion period, and the collision part is made of heat-resistant and wear-resistant material such as ceramic material, and the collision part is mounted on the top surface of the piston or inside the cavity. This is what I did.

また、特開昭61−1710号公報に開示された直噴火
花点火多種燃料内燃機関は、噴射弁よりの噴霧角をmm
し、燃料主噴流をピストン下死点近傍にあるピストンキ
ャビティ内に到達せしめるようにし、キャビティ内に予
混合気を形成し、キャビテイ外に空気層を形成した層状
給気を構築するものである。
Furthermore, a direct injection spark ignition multi-fuel internal combustion engine disclosed in Japanese Patent Application Laid-open No. 1710/1983 has a spray angle from an injection valve of mm.
Then, the main fuel jet is made to reach the piston cavity near the bottom dead center of the piston, a premixed air mixture is formed in the cavity, and a stratified air supply is created with an air layer formed outside the cavity.

〔発明が解決しようとする課題〕[Problem to be solved by the invention]

ところで、上記03KA型の燃焼室を備えたピストンを
用いたエンジンは、単孔ノズルから噴射された燃料を衝
突させる衝突面はピストンヘッドの平らな衝突面であり
、燃料が該衝突面に衝突して円盤状に拡散するが、ピス
トンの上昇行程によって燃焼室内へのスキツシユ流が発
生し、該スキッシュ流によって薄膜円盤状の燃料と空気
と良好な混合気を生成して燃焼状態を良好にするもので
ある。しかしながら、N Oxの発生を低減するため、
燃料噴射ノズルから噴射される燃料の噴射時期を遅らせ
ると、燃焼室に発生する逆スキッシュ流のため、スキン
シュ流が弱められ、燃料噴流と良好な混合が損なわれ、
燃焼の悪化が避けられないという問題がある。
By the way, in an engine using a piston equipped with the above-mentioned 03KA type combustion chamber, the collision surface on which the fuel injected from the single-hole nozzle collides is a flat collision surface of the piston head, and the fuel collides with the flat collision surface of the piston head. However, due to the upward stroke of the piston, a squish flow is generated into the combustion chamber, and this squish flow creates a thin film disc-shaped mixture of fuel and air to improve combustion conditions. It is. However, in order to reduce the generation of NOx,
If the injection timing of the fuel injected from the fuel injection nozzle is delayed, the squish flow will be weakened due to the reverse squish flow generated in the combustion chamber, and good mixing with the fuel jet will be impaired.
There is a problem that deterioration of combustion cannot be avoided.

また、前掲特開昭63−120815号公報に開示され
た燃料噴射式内燃機関は、衝突面を断熱構造に構成して
メタノールの気化を促進するものであるが、上記と同様
な問題を解決できるものではない。
Furthermore, the fuel injection internal combustion engine disclosed in the above-mentioned Japanese Patent Application Laid-Open No. 63-120815 has a collision surface with a heat-insulating structure to promote vaporization of methanol, but it can solve the same problem as above. It's not a thing.

また、前掲特開昭62−139921号公報及び特開昭
63−1710号公報に開示されたものについても、上
記公報に開示されたものと同様に、逆スキンシュ流のた
めスキッシュ流が弱められるという問題に対する対策は
講じられていない。
In addition, the squish flow is said to be weakened due to the reverse squish flow, similar to that disclosed in the above-mentioned Japanese Patent Application Laid-Open Nos. 62-139921 and 1988-1710. No measures have been taken to address the problem.

この発明の目的は、上記の課題を解決することであり、
ピストンヘッドに形成したキャビティ即ち燃焼室内で噴
射時期を遅らせて噴射した燃料と空気とで混合気を生成
させて良好に燃焼させるのに、スキッシュ流を逆方向に
ガイドする通路をピストンヘッドとシリンダヘッド下面
とで形成し、燃焼室内に平坦面を備えた突起体を配置し
、該平坦面に燃料噴射ノズルから燃料を噴射し、その噴
射した液状燃料を前記被膜に衝突させて、円盤状に均一
に拡散させ、燃焼室内にガイド通路を通してスキンシュ
流で流入した空気の流れ方向と円盤状に拡散して噴射さ
れる燃料の燃料噴射方向とをほぼ直交状態に交叉させて
混合を促進させ、燃料噴射ノズルからの燃料の噴射時期
を遅らせても逆スキンシュ流でスキッシュ流が弱められ
る現象を避け、No工の発生を低減し、良好な燃焼を行
わせて未燃燃料或いは中間生成物の排出を防止する燃料
衝突拡散式エンジンを提供することである。
The purpose of this invention is to solve the above problems,
In order to generate a mixture between the injected fuel and air by delaying the injection timing in the cavity formed in the piston head, that is, the combustion chamber, and achieve good combustion, the piston head and cylinder head are designed to create a passage that guides the squish flow in the opposite direction. A protrusion formed with a lower surface and having a flat surface is disposed inside the combustion chamber, and fuel is injected from a fuel injection nozzle onto the flat surface, and the injected liquid fuel collides with the coating to form a uniform disc-shape. The flow direction of the air flowing into the combustion chamber in a skinsch flow through the guide passage and the fuel injection direction of the fuel diffused and injected in a disk shape are made to intersect in a nearly perpendicular state to promote mixing and fuel injection. Even if the injection timing of fuel from the nozzle is delayed, it avoids the phenomenon where the squish flow is weakened by the reverse squish flow, reduces the occurrence of No. 1, performs good combustion, and prevents the emission of unburned fuel or intermediate products. It is an object of the present invention to provide a fuel impingement diffusion type engine.

〔課題を解決するための手段〕[Means to solve the problem]

この発明は、上記目的を達成するため、次のように構成
されている。即ち、この発明は、ピストンへノドに形成
した燃焼室、該燃焼室のほぼ中央底部に設けた突起体、
該突起体に対向して噴口を開口するシリンダヘッドに取
付けた燃料噴射ノズル、前記噴口から噴射された液状燃
料を衝突させる前記突起体の頂面に形成した平坦面、シ
リンダヘッド下面から前記燃焼室内へ突出可能であり且
つスキンシュ流をガイドしてスキッシュ流の方向を変更
する突出部を有する燃料衝突拡散式エンジンに関する。
In order to achieve the above object, the present invention is configured as follows. That is, the present invention includes a combustion chamber formed at the throat of the piston, a protrusion provided at the substantially central bottom of the combustion chamber,
A fuel injection nozzle attached to a cylinder head that opens a nozzle facing the protrusion, a flat surface formed on the top surface of the protrusion that causes the liquid fuel injected from the nozzle to collide with the fuel injection nozzle, and a flat surface formed on the top surface of the protrusion that causes the liquid fuel injected from the nozzle to collide with the fuel injection nozzle, which is injected into the combustion chamber from the bottom surface of the cylinder head. The present invention relates to a fuel impingement-diffusion engine having a protrusion that can protrude into the air and guide a squish flow to change the direction of the squish flow.

また、この燃料衝突拡散式エンジンにおいて、前記突出
部はピストン上死点で前記燃焼室内へ突出した状態で、
前記突出部と前記燃焼室の周壁とで環状円錐状通路を形
成するものである。
Further, in this fuel collision diffusion type engine, the protruding portion is in a state of protruding into the combustion chamber at the piston top dead center,
The protrusion and the peripheral wall of the combustion chamber form an annular conical passage.

更に、この燃料衝突拡散式エンジンにおいて、前記燃料
噴射ノズルから噴射される燃料の噴射時期を遅らせるも
のである。
Furthermore, in this fuel collision diffusion type engine, the injection timing of the fuel injected from the fuel injection nozzle is delayed.

[作用〕 この発明による燃料衝突拡散式エンジンは、上記のよう
に構成され、次のように作用する。即ち、この燃料衝突
拡散式エンジンは、ピストンヘッドに形成した燃焼室の
ほぼ中央底部に突起体を設け、該突起体に対向して噴口
を開口する燃料噴射ノズルをシリンダヘッドに取付け、
前記噴口がら噴射された液状燃料を衝突させる平坦面を
前記突起体の頂面に形成し、特に、シリンダヘッド下面
から前記燃焼室側へ突出させた突出部をピストン上死点
で前記燃焼室内に突出可能に構成し、前記燃焼室の壁面
との間に環状円錐状通路を形成し、前記突出部によって
スキッシュ流をガイドしてスキンシュ流の方向を積掻的
に変更し、前記環状円錐状通路によってスキッシュ流を
前記燃焼室の壁面に沿って流動させ、逆スキンシュ流が
発生しても該逆スキフシュ流によるスキンシュ流の流れ
を弱める作用を抑制する。
[Operation] The fuel impingement diffusion engine according to the present invention is constructed as described above and operates as follows. That is, in this fuel collision diffusion type engine, a protrusion is provided at approximately the center bottom of the combustion chamber formed in the piston head, and a fuel injection nozzle with a nozzle opening facing the protrusion is attached to the cylinder head.
A flat surface is formed on the top surface of the protrusion, on which the liquid fuel injected from the nozzle collides, and in particular, a protrusion that protrudes from the lower surface of the cylinder head toward the combustion chamber is inserted into the combustion chamber at the top dead center of the piston. an annular conical passageway is formed between the combustion chamber and the wall surface of the combustion chamber, the protrusion guides the squish flow to constructively change the direction of the squish flow; This causes the squish flow to flow along the wall surface of the combustion chamber, and even if a reverse squish flow occurs, the effect of weakening the flow of the squish flow due to the reverse squish flow is suppressed.

一方、前記燃料噴射ノズルから噴射された燃料は前記平
坦面に液状で衝突して該平坦面に沿って半径方向外向き
に拡散し、円盤状燃料薄膜を形成するが、前記突出部に
ガイドされたスキッシュ流を前記円盤状燃料薄膜にスキ
ッシュ流を交差させることができ、燃料と空気との良好
な混合を実現し、燃焼効率の向上を図ることができる。
On the other hand, the fuel injected from the fuel injection nozzle collides with the flat surface in liquid form and diffuses radially outward along the flat surface to form a disc-shaped fuel thin film, but the fuel is not guided by the protrusion. The squish flow can be caused to intersect with the disc-shaped thin fuel film, thereby achieving good mixing of fuel and air and improving combustion efficiency.

従って、前記燃料噴射ノズルから噴射される燃料の噴射
時期を遅らせても、スキンシ流は逆スキフシュ流で弱め
られることがなく、円盤状燃料薄膜と交差して良好な混
合が達成できる。
Therefore, even if the injection timing of the fuel injected from the fuel injection nozzle is delayed, the squish flow is not weakened by the reverse skiff flow, and good mixing can be achieved by intersecting with the disc-shaped fuel thin film.

〔実施例〕〔Example〕

以下、図面を参照して、この発明による燃料衝突拡散式
エンジンの実施例を説明する。
Embodiments of the fuel collision-diffusion engine according to the present invention will be described below with reference to the drawings.

第1[fflはこの発明による燃料衝突拡散式エンジン
の一実施例を示す断面図、及び第2図は第1図の符号A
の部分の拡大説明図である。
1 [ffl is a sectional view showing an embodiment of the fuel collision diffusion type engine according to the present invention, and FIG.
FIG.

第1図に示すように、この燃料衝突拡散式エンジンは、
シリンダブロック9、該シリンダブロック9に固定され
た吸気ポート6及び排気ボート7を備えてシリンダへノ
ド3、シリンダブロック9の孔部に嵌合したシリンダラ
イナ14、及び該シリンダライナ14内を往復運動する
ピストン15を有している。1気ボート6には吸気弁1
6が配置され、また排気ポート7には排気弁I7が配置
されている。ピストン15は、例えば、アルミニウム等
の金属材料から成り、ピストン15のピストンヘッド1
には、キャビティ即ち燃焼室2が形成されている。特に
、このピストンヘッド1に形成した燃焼室2については
、はぼ中央底部に上方に伸びる突起体5が形成されてい
る。この突起体5は、例えば、断熱性に冨んだジルコニ
ア(ZrOl)等のセラミックスから製作した1板を取
付けることができる。突起体5の上部は、キャビティ底
面から上方に伸びて燃焼室2の開口部100面即ちピス
トンヘッド1の頂面より下方に位置している。この突起
体5の頂面ば平坦面12に形成されている。この平坦面
12は、液状燃料が衝突する衝突面を構成する。
As shown in Figure 1, this fuel impingement-diffusion engine is
A cylinder block 9, an intake port 6 and an exhaust boat 7 fixed to the cylinder block 9, a nozzle 3 to the cylinder, a cylinder liner 14 fitted into a hole in the cylinder block 9, and reciprocating movement within the cylinder liner 14. It has a piston 15 that does. Intake valve 1 for 1-air boat 6
6 is disposed, and an exhaust valve I7 is disposed at the exhaust port 7. The piston 15 is made of a metal material such as aluminum, and the piston head 1 of the piston 15 is made of a metal material such as aluminum.
A cavity or combustion chamber 2 is formed therein. In particular, regarding the combustion chamber 2 formed in the piston head 1, a protrusion 5 extending upward is formed at the center bottom of the piston head. For example, a plate made of ceramic such as zirconia (ZrOl) with high heat insulation properties can be attached to the protrusion 5. The upper part of the protrusion 5 extends upward from the bottom surface of the cavity and is located below the opening 100 surface of the combustion chamber 2, that is, the top surface of the piston head 1. The top surface of this protrusion 5 is formed into a flat surface 12. This flat surface 12 constitutes a collision surface on which the liquid fuel collides.

また、シリンダヘッド3には、ピストンへ、ド1に形成
した燃焼室2に対向して下方に伸びる突出部8が形成さ
れている。この突出部8は、下部が断面積が大きくなる
拡大突出部となり、ピストン上死点で燃焼室2内へ突出
した状態になる。他方、燃焼室2に設けた突起体5の平
坦面】2に対向して噴口11を開口する燃料噴射ノズル
4が取付けられている。燃料噴射ノズル4は、ビントル
ノズル等の噴射ノズルから成り、該噴射ノズルの噴口1
1から噴射された燃料が液状で平坦面12の中央部に衝
突するように構成されている。
Further, the cylinder head 3 is formed with a protrusion 8 extending downward toward the piston and facing the combustion chamber 2 formed in the cylinder 1 . This protruding portion 8 becomes an enlarged protruding portion whose lower portion has a larger cross-sectional area, and is in a state of protruding into the combustion chamber 2 at the piston top dead center. On the other hand, a fuel injection nozzle 4 having a nozzle opening 11 facing the flat surface 2 of the protrusion 5 provided in the combustion chamber 2 is attached. The fuel injection nozzle 4 consists of an injection nozzle such as a bottle nozzle, and the injection nozzle 1
The structure is such that the fuel injected from 1 collides with the center of the flat surface 12 in liquid form.

従って、シリンダヘッド3に設けた突出部8は、第2図
に明瞭に示すように、ピストンヘッド1に形成した燃焼
室2を構成するキャビティの拡がり即ち燃焼室2の周壁
に対応して下方に向かって断面積が拡大しており、ピス
トン上死点では突出部8と燃焼室2の周壁即ち壁面19
とで環状円錐状通路13を形成する。従って、ピストン
の上昇によって発生する燃焼室2へのスキ・2シユ流は
、突出部8の外周面18にガイドされて矢印のように噴
流方向が変更され、燃焼室2の壁面19に沿って旋回流
れとなる。そこで、このスキッシュ流の旋回流れは、燃
料噴射ノズル4の噴口11から噴射された液状燃料に対
して直交状Sに交差し、空気と燃料の混合が促進される
。それ故に、N OXの発生を防止するため、燃料噴射
ノズル4から噴射される燃料の噴射時期を遅らせたとし
ても、突出部8にガイドされたスキッシュ流は逆スキッ
シュ流に抵抗することなく、スキッシュ流の旋回流れが
弱められるような現象は発生しない。
Therefore, as clearly shown in FIG. 2, the protruding portion 8 provided on the cylinder head 3 extends downward corresponding to the expansion of the cavity forming the combustion chamber 2 formed in the piston head 1, that is, the peripheral wall of the combustion chamber 2. The cross-sectional area increases in the direction, and at the top dead center of the piston, the protrusion 8 and the peripheral wall of the combustion chamber 2, that is, the wall surface 19
and form an annular conical passage 13. Therefore, the jet flow generated by the rising of the piston into the combustion chamber 2 is guided by the outer circumferential surface 18 of the protrusion 8, and the jet direction is changed as shown by the arrow, and the jet flow is directed along the wall surface 19 of the combustion chamber 2. It becomes a swirling flow. Therefore, the swirling flow of the squish flow intersects the liquid fuel injected from the injection port 11 of the fuel injection nozzle 4 at right angles S, thereby promoting the mixing of air and fuel. Therefore, even if the injection timing of the fuel injected from the fuel injection nozzle 4 is delayed in order to prevent the generation of NOx, the squish flow guided by the protrusion 8 will not resist the reverse squish flow and will continue to squish. A phenomenon that weakens the swirling flow of the flow does not occur.

この発明による燃料衝突拡散式エンジンは、上記のよう
に構成されており、次のように作用する。
The fuel collision diffusion type engine according to the present invention is constructed as described above and operates as follows.

この燃料衝突拡散式エンジンは、シリンダヘッド3に取
付けた燃料噴射ノズル4の噴口11から低圧で噴射され
た燃料は、棒状の液状燃料として噴口11に対向した燃
焼室2内の突起体5の平坦面12に衝突し、薄い膜状の
円盤状になって半径方向外向きに拡散する。この時、ピ
ストン1の上昇で発生するスキッシュ流は、シリンダヘ
ッド3に設けた突出部8の外周面18にガイドされて環
状円錐状通路13を通って燃焼室2内に流入し、次いで
、燃焼室2の壁面19と突起体5の壁面20に沿って旋
回流れを形成する。そこで、該スキッシュ流と円盤状薄
膜燃料と直交状態に交差して良好な混合を実現すること
ができ、良好な燃焼状態を確保して燃焼効率を向上でき
る。
In this fuel collision diffusion type engine, fuel injected at low pressure from a nozzle 11 of a fuel injection nozzle 4 attached to a cylinder head 3 is converted into a rod-shaped liquid fuel into a flat protrusion 5 in a combustion chamber 2 facing the nozzle 11. It impinges on surface 12 and diffuses radially outward in the form of a thin film-like disk. At this time, the squish flow generated by the rise of the piston 1 is guided by the outer peripheral surface 18 of the protrusion 8 provided on the cylinder head 3, flows into the combustion chamber 2 through the annular conical passage 13, and then combusts A swirling flow is formed along the wall surface 19 of the chamber 2 and the wall surface 20 of the projection body 5. Therefore, the squish flow intersects the disk-shaped thin film fuel in a perpendicular state to achieve good mixing, thereby ensuring a good combustion state and improving combustion efficiency.

通常、NOXの発生を低減するため、燃料噴射ノズル4
から燃焼室2に噴射される燃料の噴射時期を遅らせるが
、従来の燃焼室の構造であると、噴射時期を遅らせると
、燃焼室へのスキッシュ流は逆スキッシュ流のため、ス
キ、シュ流の流れが弱められ、燃料噴流との良好な混合
作用が損なわれ、燃焼の悪化を引き起こす原因となる。
Normally, in order to reduce the generation of NOx, the fuel injection nozzle 4
However, with the conventional combustion chamber structure, if the injection timing is delayed, the squish flow into the combustion chamber is a reverse squish flow, so the squish flow into the combustion chamber is reversed. The flow is weakened and good mixing with the fuel jet is impaired, causing poor combustion.

しかしながら、この燃料衝突拡散式エンジンでは、シリ
ンダヘッド3の下面部にスキッシュ流の流れ方向を変更
するガイドとなる突出部8を設けたので、燃焼室2のス
キッシュ流で流入した空気流れは、燃焼室2内で旋回流
れの向きが通常の流れ即ち燃焼室2の外側部から中央部
へ向かう流れとは逆の流れ方向に変更され、逆スキッシ
ュ流が発生しても該逆スキッシュ流でスキッシュ流の旋
回流れが妨げられることがなく、円盤状燃料噴流と空気
とは良好な混合が維持され、噴射時期を遅らせたとして
も、燃焼状態が悪化することが避けられる。従って、燃
料噴射ノズル4の噴口11から噴射された液状の燃料は
、突起体5の平坦面12に衝突して直ちに該平坦面12
に沿って半径方向に拡がって円盤形状のフィルムとなっ
て均一に拡散する。そこで、この円盤状フィルムの燃料
は、ピストン1の上昇行程に伴って発生する燃焼室2へ
のスキッシュ流とは直交状態に交叉し、混合が促進され
ると共に、直ちに着火燃焼することができる。
However, in this fuel impingement diffusion type engine, a protrusion 8 is provided on the lower surface of the cylinder head 3 to serve as a guide for changing the flow direction of the squish flow. Even if the direction of the swirling flow in the chamber 2 is changed to the opposite flow direction from the normal flow, that is, the flow from the outside part to the center part of the combustion chamber 2, and a reverse squish flow occurs, the reverse squish flow is a squish flow. The swirling flow of the fuel jet is not obstructed, and good mixing between the disk-shaped fuel jet and the air is maintained, and even if the injection timing is delayed, deterioration of the combustion state can be avoided. Therefore, the liquid fuel injected from the nozzle 11 of the fuel injection nozzle 4 collides with the flat surface 12 of the protrusion 5 and immediately
It spreads in the radial direction along the , becoming a disk-shaped film and spreading uniformly. Therefore, the fuel in this disc-shaped film intersects perpendicularly with the squish flow into the combustion chamber 2 that occurs with the upward stroke of the piston 1, promoting mixing and allowing immediate ignition and combustion.

〔発明の効果〕〔Effect of the invention〕

この発明による燃料衝突拡散式エンジンは、上記のよう
に構成されており、次のような効果を有する。即ち、こ
の燃料衝突拡散式エンジンは、ピストンヘッドに形成し
た燃焼室、該燃焼室のほぼ中央底部に設けた突起体、該
突起体に対向して噴口を開口するシリンダヘッドに取付
けた燃料噴射ノズル、前記噴口から噴射された液状燃料
を衝突させる前記突起体の頂面に形成した平坦面、シリ
ンダへノド下面から前記燃焼室内へ突出可能であり且つ
スキッシュ流をガイドしてスキッシュ流の方向を変更す
る突出部を有するので、前記突出部によってスキッシュ
流をガイドしてスキッシュ流の方向を積極的即ち強制的
に変更し、前記突出部と前記燃焼室の壁面で形成される
環状円錐状通路によってスキッシュ流を前記燃焼室の壁
面及び前記突起体の壁面に沿って流動して旋回流れを形
成し、逆スキッシュ流によるスキッシュ流の流れを弱め
る作用を抑制する。従って、逆スキッシュ流が生じても
スキンシュ流での旋回流れが弱まることがないので、噴
霧と空気とは良好な混合を維持し、噴射時期を遅らせた
ときも燃焼の悪化を避けることができる。
The fuel collision diffusion type engine according to the present invention is configured as described above, and has the following effects. That is, this fuel collision diffusion type engine includes a combustion chamber formed in a piston head, a protrusion provided at approximately the center bottom of the combustion chamber, and a fuel injection nozzle attached to the cylinder head with a nozzle opening facing the protrusion. , a flat surface formed on the top surface of the protrusion that collides the liquid fuel injected from the nozzle, which can protrude into the combustion chamber from the lower surface of the throat of the cylinder, and guides the squish flow to change the direction of the squish flow. Since the projection has a protrusion that guides the squish flow and positively or forcibly changes the direction of the squish flow, the annular conical passage formed by the protrusion and the wall surface of the combustion chamber guides the squish flow. The flow is caused to flow along the wall surface of the combustion chamber and the wall surface of the protrusion to form a swirling flow, thereby suppressing the effect of weakening the squish flow due to the reverse squish flow. Therefore, even if a reverse squish flow occurs, the swirling flow in the squish flow is not weakened, so that good mixing of the spray and air can be maintained, and deterioration of combustion can be avoided even when the injection timing is delayed.

一方、前記燃料噴射ノズルから噴射された燃料は前記平
坦面に液状で衝突して円盤状燃料薄膜を形成するが、前
記突出部にガイドされたスキンシュ流を前記円盤状燃料
薄膜にスキッシュ流を交差させることができ、良好な混
合を実現し、燃焼効率の向上を図ることができる。
On the other hand, the fuel injected from the fuel injection nozzle collides with the flat surface in liquid form to form a disc-shaped fuel thin film, and the squish flow guided by the protrusion crosses the disc-shaped fuel film. It is possible to achieve good mixing and improve combustion efficiency.

従って、前記燃料噴射ノズルから噴射される燃料の噴射
時期を遅らせても、スキッシュ流は逆スキッシュ流で弱
められることがなく、円盤状燃料′iR膜と交差して良
好な混合が達成できる。
Therefore, even if the injection timing of the fuel injected from the fuel injection nozzle is delayed, the squish flow is not weakened by the reverse squish flow, and good mixing can be achieved by crossing the disk-shaped fuel 'iR film.

また、前記突出部はピストン上死点で前記燃焼室内へ突
出した状態で、前記突出部と前記燃焼室の周壁とで環状
円錐状通路を形成するので、ピストン上昇で発生するス
キッシュ流は、前記環状円錐状通路に確実にガイドされ
、前記燃焼室の周壁に沿って燃焼室の外側から中央部へ
と流れ、逆スキンシュ流と衝突することが避けられ、円
盤状燃料薄膜と交差して良好に混合される。
Further, when the protrusion protrudes into the combustion chamber at the top dead center of the piston, the protrusion and the peripheral wall of the combustion chamber form an annular conical passage. It is reliably guided by the annular conical passage, flows from the outside to the center of the combustion chamber along the peripheral wall of the combustion chamber, avoids colliding with the reverse skinsh flow, and crosses the disk-shaped thin fuel film to form a good flow. mixed.

また、前記燃料噴射ノズルから噴射される燃料の噴射時
期を遅らせるので、スキッシュ流が逆スキフシュ流で弱
められることなく、NOxの発生を抑制する燃焼を行わ
せることができる。
Furthermore, since the injection timing of the fuel injected from the fuel injection nozzle is delayed, the squish flow is not weakened by the reverse squish flow, and combustion that suppresses the generation of NOx can be performed.

従って、前記被膜の衝突面は常に清らがな衝突面と提供
でき、該被膜に衝突した液状燃料は常に良好に該衝突面
に沿って半径方向外向きに拡散することができ、燃料は
好ましい薄膜円盤状に拡散する。
Therefore, the impingement surface of the coating can always be provided with a clean impingement surface, and the liquid fuel impinged on the coating can always be well diffused radially outward along the impingement surface, and the fuel is preferably Diffuses into a thin film disc.

【図面の簡単な説明】[Brief explanation of drawings]

第1図はこの発明による燃料衝突拡散式エンジンの一実
施例を示す断面図、及び第2図は第1図の符号Aの部分
の拡大説明図である。 1−  ピストンヘッド、2−−−燃焼室、3シリンダ
ヘツド、4− 燃料噴射ノズル、5突起体、8− 突出
部、10 =−燃焼室の開口部、11− 噴口、12−
平坦面、13− 環状円錐状通路。 出願人  いす\自動車株式会社 代理人  弁理士 尾 仲 −宗
FIG. 1 is a sectional view showing an embodiment of a fuel impingement diffusion type engine according to the present invention, and FIG. 2 is an enlarged explanatory view of a portion indicated by reference numeral A in FIG. 1- Piston head, 2-- Combustion chamber, 3- Cylinder head, 4- Fuel injection nozzle, 5 Projection, 8- Projection, 10 =- Opening of combustion chamber, 11- Nozzle port, 12-
flat surface, 13- annular conical passage; Applicant: Isu\Jidosha Co., Ltd., Patent Attorney: So Naka Onaka

Claims (3)

【特許請求の範囲】[Claims] (1)ピストンヘッドに形成した燃焼室、該燃焼室のほ
ぼ中央底部に設けた突起体、該突起体に対向して噴口を
開口するシリンダヘッドに取付けた燃料噴射ノズル、前
記噴口から噴射された液状燃料を衝突させる前記突起体
の頂面に形成した平坦面、シリンダヘッド下面から前記
燃焼室内へ突出可能であり且つスキッシュ流をガイドし
てスキッシュ流の方向を変更する突出部を有する燃料衝
突拡散式エンジン。
(1) A combustion chamber formed in the piston head, a protrusion provided at the bottom of the combustion chamber in the center, a fuel injection nozzle attached to the cylinder head with a nozzle opening facing the protrusion, and a fuel injection nozzle that is injected from the nozzle. Fuel collision/diffusion having a flat surface formed on the top surface of the protrusion that collides the liquid fuel, and a protrusion that can protrude into the combustion chamber from the lower surface of the cylinder head and guides the squish flow and changes the direction of the squish flow. formula engine.
(2)前記突出部はピストン上死点で前記燃焼室内へ突
出した状態で、前記突出部と前記燃焼室の周壁とで環状
円錐状通路を形成する請求項1に記載の燃料衝突拡散式
エンジン。
(2) The fuel impingement-diffusion engine according to claim 1, wherein the protrusion protrudes into the combustion chamber at the top dead center of the piston, and the protrusion and the peripheral wall of the combustion chamber form an annular conical passage. .
(3)前記燃料噴射ノズルから噴射される燃料の噴射時
期を遅らせる請求項1に記載の燃料衝突拡散式エンジン
(3) The fuel impingement diffusion engine according to claim 1, wherein the injection timing of the fuel injected from the fuel injection nozzle is delayed.
JP2112645A 1990-04-30 1990-04-30 Fuel collision diffusion type engine Pending JPH0412122A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2112645A JPH0412122A (en) 1990-04-30 1990-04-30 Fuel collision diffusion type engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2112645A JPH0412122A (en) 1990-04-30 1990-04-30 Fuel collision diffusion type engine

Publications (1)

Publication Number Publication Date
JPH0412122A true JPH0412122A (en) 1992-01-16

Family

ID=14591918

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2112645A Pending JPH0412122A (en) 1990-04-30 1990-04-30 Fuel collision diffusion type engine

Country Status (1)

Country Link
JP (1) JPH0412122A (en)

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